Shaft Stress Calculations - EDGEedge.rit.edu/edge/P07202/public/Mechanical/Documentation... ·...

24
CALCULATIONS AND ANALYSIS See Stress Calculation Spreadsheet for sources of equations, sources of constants and material properties, and additional calculations Impact Analysis Direct wheel impact at max speed By using the deflection equation, EI Fl s 192 3 (based upon two fully constrained rod ends), solving for F, and using a basic kinematic equation ( ) ( 2 2 2 s a v v o f ) to solve for s in terms of F, the force of impact can be determined (227505 N) Utilizing shaft stress equations shown below the stress can be determined (400 MPa) When comparing this to the shaft’s yield strength, a factor of safety of 1.33 is calculated

Transcript of Shaft Stress Calculations - EDGEedge.rit.edu/edge/P07202/public/Mechanical/Documentation... ·...

Page 1: Shaft Stress Calculations - EDGEedge.rit.edu/edge/P07202/public/Mechanical/Documentation... · Shaft Stress Calculations Shaft 1 (Diameter=3 ... 1 = 2.25E12 cycles to failure Shaft

CALCULATIONS AND ANALYSIS

See Stress Calculation Spreadsheet for sources of equations,

sources of constants and material properties, and additional

calculations

Impact Analysis

Direct wheel impact at max speed

By using the deflection equation, EI

Fls

192

3

(based upon two fully constrained

rod ends), solving for F, and using a basic kinematic equation ( )(222

savv of

) to solve for s in terms of F, the force of impact can be determined (227505 N)

Utilizing shaft stress equations shown below the stress can be determined (400

MPa)

When comparing this to the shaft’s yield strength, a factor of safety of 1.33 is

calculated

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Direct pulley impact at max speed

Utilizing this same force and finding the stress on the shaft due to bending.

I

Mc=8510 MPa

This means the shaft will permanently bend due to the moment applied on it

The way to avoid this catastrophic failure is to ensure the chassis protects these

open gears by extending past its edges or enclosing it completely. While this may

not completely ensure the module’s safety, it will fix nearly every probable

scenario.

Shaft Stress Calculations

Shaft 1 (Diameter=3/8”)

Material: 1045 Steel, Yield Strength (Sy)= 530 MPa, Ultimate Strength= 625MPa

Max Stress

o The shaft is keyed for a 3/32” key, thus a close approximation for the actual

yield strength is ¾ the materials yield strength (Keyed Yield Strength=398

MPa)

o Loading is comprised of three components

Moment-Based on cantilevered distance from bearing and radial load

exerted on shaft from the miter gear (2.1 N-m)

Force- Based on axial load exerted on shaft from miter gear (156.12

N)

Torque- Exerted by the stall torque of the motor, through a gear ratio

of 2:1 (9.64 N-m)

o Stress Calculation-

2/122

max ]48)8[(4

TFdMd

=102 MPa

2/122

3max ]64)8[(2

TFdMd

= 58.4 MPa

o Factors of Safety-

max

ySn = 3.9

max2

ySn = 3.4

Fatigue Life

o Infinite Life- 2000RPM (Average operating speed)=33.3 cycles/second

5 year life @ 1 hour operating time (2 hr per week)-approximately

1,908,000 seconds of use

33.3*1,908,000=6.4E7 cycles to failure for infinite life

o The endurance strength can be calculated using the stress concentration

factors from the keyway (197 MPa)

o ’F=Sut+345MPa= 970 MPa

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o )2log(

)/'log(

e

eF

N

Sb =-0.109915548

o b

ut

F

Sf )102(

' 3 =.673

o e

ut

S

Sfa

2)(=900 MPa

o Loads are based on typical operating conditions, not max conditions

Moment-Based on cantilevered distance from bearing and radial load

exerted on shaft from the miter gear (2.1 N-m)

Force- Based on axial load exerted on shaft from miter gear (156.12

N)

Torque- Exerted by the operating torque of the motor, through a gear

ratio of 2:1 (2.82 N-m)

o 2/122

3]48)8[(

4TFdM

da = 39.4 MPa

o b

a

aN

1

= 2.25E12 cycles to failure

Shaft 2 (Diameter=1/2”)

Material: 1045 Steel, Yield Strength= 530 MPa, Ultimate Strength= 625MPa

Max Stress

o The shaft is keyed for a 1/8” key, thus the actual yield strength can be equated

to ¾ the materials yield strength (Keyed Yield Strength=398 MPa)

o Loading is comprised of three components

Moment-Based on the axle length between bearings and radial load

exerted on shaft from the miter gear (4.28 N-m)

Force- Based on axial load exerted on shaft from miter gear (156.12

N)

Torque- Exerted by the stall torque of the motor, through a gear ratio

of 2:1 (9.64 N-m)

o Stress Calculation-

2/122

max ]48)8[(4

TFdMd

= 47.2 MPa

2/122

3max ]64)8[(2

TFdMd

= 26.5 MPa

o Factors of Safety-

max

ySn = 8.4

max2

ySn = 7.5

Fatigue Life

o Infinite Life- 1000RPM=16.67 cycles/second

Page 4: Shaft Stress Calculations - EDGEedge.rit.edu/edge/P07202/public/Mechanical/Documentation... · Shaft Stress Calculations Shaft 1 (Diameter=3 ... 1 = 2.25E12 cycles to failure Shaft

5 year life @ 1 hour operating time (2 hr per week)-approximately

1,908,000 seconds of use

16.67*1,908,000=3.2E7 cycles to failure for infinite life

o The endurance strength can be calculated using the stress concentration

factors from the keyway (197 MPa)

o ’F=Sut+345MPa= 970 MPa

o )2log(

)/'log(

e

eF

N

Sb =-0.109915548

o b

ut

F

Sf )102(

' 3 =.673

o e

ut

S

Sfa

2)(=900 MPa

o Loads are based on typical operating conditions, not max conditions

Moment-Based on the axle length between bearings and radial load

exerted on shaft from the miter gear (4.28 N-m)

Force- Based on axial load exerted on shaft from miter gear (156.12

N)

Torque- Exerted by the operating torque of the motor, through a gear

ratio of 2:1 (2.82 N-m)

o 2/122

3]48)8[(

4TFdM

da = 25.6 MPa

o b

a

aN

1

= 1.15E14 cycles to failure

Shaft 3 (Diameter=3/4”)

Material: 1045 Steel, Yield Strength= 530 MPa, Ultimate Strength= 625MPa

Max Stress

o The shaft is keyed for a 3/16” key, thus the actual yield strength can be

equated to ¾ the materials yield strength (Keyed Yield Strength=398 MPa)

o Loading is comprised of three components

Moment-Based on the axle length between bearings and the force

exerted by the weight of the system (21.53 N-m)

Force- Based on axial load exerted on the shaft from turning forces

(235.44 N)

Torque- Exerted by the stall torque of the motor, through a gear ratio

of 8:1 (38.56 N-m)

o Stress Calculation-

2/122

max ]48)8[(4

TFdMd

= 59.0 MPa

2/122

3max ]64)8[(2

TFdMd

= 32.7 MPa

o Factors of Safety-

Page 5: Shaft Stress Calculations - EDGEedge.rit.edu/edge/P07202/public/Mechanical/Documentation... · Shaft Stress Calculations Shaft 1 (Diameter=3 ... 1 = 2.25E12 cycles to failure Shaft

max

ySn = 6.7

max2

ySn = 6.1

Fatigue Life

o Infinite Life- 500RPM=8.34 cycles/second

5 year life @ 1 hour operating time (2 hr per week)-apprx 1,908,000

seconds of use

8.34*1,908,000=1.6E7 cycles to failure for infinite life

o The endurance strength can be calculated using the stress concentration

factors from the keyway (197 MPa)

o ’F=Sut+345MPa= 970 MPa

o )2log(

)/'log(

e

eF

N

Sb =-0.109915548

o b

ut

F

Sf )102(

' 3 =.673

o e

ut

S

Sfa

2)(=900 MPa

o Loads are based on typical operating conditions, not max conditions

Moment-Based on the axle length between bearings and the force

exerted by the weight of the system (21.53 N-m)

Force- Based on axial load exerted on the shaft from turning forces

(235.4 N)

Torque- Exerted by the operating torque of the motor, through a gear

ratio of 8:1 (11.28 N-m)

o 2/122

3]48)8[(

4TFdM

da = 35.6 MPa

o b

a

aN

1

= 5.7E12 cycles to failure

Steering Shaft (Diameter=1/4”)

Material: 303 Stainless Steel, Yield Strength= 240 MPa, Ultimate Strength= 620 MPa

Max Stress

o Loading is based on torque alone (0.745 N-m)

o Stress Calculation-

2/122

max ]48)8[(4

TFdMd

= 25.7 MPa

2/122

3max ]64)8[(2

TFdMd

= 14.8 MPa

o Factors of Safety-

max

ySn = 9.4

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max2

ySn = 8.1

Fatigue Life

o ’F=Sut+345MPa=965E6 MPa

o )2log(

)/'log(

e

eF

N

Sb =-0.07772

o b

ut

F

Sf )102(

' 3 =.862

o e

ut

S

Sfa

2)(=914 MPa

o Load is comprised of torque alone (.745 N-m)

o 2/122

3]48)8[(

4TFdM

da = 25.7 MPa

o b

a

aN

1

= 9.3E19 cycles to failure

Spur Gears (Calculated using ANSI standards)

Driving Spur

Material- Carbon Steel, Yield Strength=76900 psi, Modulus of Elasticity=30E6

psi, Poisson’s Ratio=.29, Brunell Hardness 179

Max Bending Stress

o V

HW t 33000

= 306.8 lbf

o Ko= 1.25 - Overload Factor, based on light shocks encountered

o Kv= 1.15 - Dynamic Factor, based on quality and velocity of gears

o Ks= 1 - Size Factor

o Pd= .833” – Pitch diameter

o F= .25” – face width

o Km= 1.20 – Load-Distribution factor, based on geometry

o KB= 1 – Rim Thickness factor, based on geometry

o J= .325- Geometry factor, based on number of teeth of gears

o J

KK

F

PKKKW Bmd

svot =5357.1 psi

o max

ySn = 9.0

Endurance Stress

o

2/1

22

)11

(

1

G

G

p

p

p

E

v

E

vC =2284.7 lbf/in

2

Page 7: Shaft Stress Calculations - EDGEedge.rit.edu/edge/P07202/public/Mechanical/Documentation... · Shaft Stress Calculations Shaft 1 (Diameter=3 ... 1 = 2.25E12 cycles to failure Shaft

o Cf=1

o I=0.08- Geometry Factor

o 2/1)(I

C

FP

KKKWC

f

d

mso

tp =56972.4 psi

o Sc= 180000 psi- Repeatedly applied contact strength @ 107 cycles,

material property

o Zn=.59 - Stress cycle life factor, based on hardness and number of cycles

o CH=1 -Hardness ratio factor

o KT= 1- Temperature factor

o KR= 1 – Reliability factor

o )/( RTHNc

H

KKCZSS =1.9

o Comparable factor of safety= SH2=3.5

Driven Spur

Material- Carbon Steel, Yield Strength=76900 psi, Modulus of Elasticity=30E6

psi, Poisson’s Ratio=.29, Brunell Hardness 179

Max Bending Stress

o V

HW t 33000

= 306.7 lbf

o Ko= 1.25 - Overload Factor, based on light shocks encountered

o Kv= 1.15 - Dynamic Factor, based on quality and velocity of gears

o Ks= 1 - Size Factor

o Pd= 1.667” – Pitch diameter

o F= .25” – face width

o Km= 1.19 – Load-Distribution factor, based on geometry

o KB= 1 – Rim Thickness factor, based on geometry

o J= .389- Geometry factor, based on number of teeth of gears

o J

KK

F

PKKKW Bmd

svot =9011.0 psi

o max

ySn = 5.4

Endurance Stress

o

2/1

22

)11

(

1

G

G

p

p

p

E

v

E

vC =2284.7 lbf/in

2

o Cf=1

o I=0.08- Geometry Factor

o 2/1)(I

C

FP

KKKWC

f

d

mso

tp = 40010.7 psi

Page 8: Shaft Stress Calculations - EDGEedge.rit.edu/edge/P07202/public/Mechanical/Documentation... · Shaft Stress Calculations Shaft 1 (Diameter=3 ... 1 = 2.25E12 cycles to failure Shaft

o Sc= 180000 psi- Repeatedly applied contact strength @ 107 cycles,

material property

o Zn=.60 - Stress cycle life factor, based on hardness and number of cycles

o CH=1 -Hardness ratio factor

o KT= 1- Temperature factor

o KR= 1 – Reliability factor

o )/( RTHNc

H

KKCZSS = 2.70

o Comparable factor of safety= SH2=7.2

Ring/Pinion Gears (Calculated using ANSI standards)

Steering Spur

Material- 2024-T4 Aluminum, Yield Strength=47000 psi, Modulus of

Elasticity=10.4E6 psi, Poisson’s Ratio=.333

Max Bending Stress

o V

HW t 33000

= 39.3 lbf

o Ko= 1.25 - Overload Factor, based on light shocks encountered

o Kv= 1.10 - Dynamic Factor, based on quality and velocity of gears

o Ks= 1 - Size Factor

o Pd= .4375” – Pitch diameter

o F= .125” – face width

o Km= 1.20 – Load-Distribution factor, based on geometry

o KB= 1 – Rim Thickness factor, based on geometry

o J= .24- Geometry factor, based on number of teeth of gears

o J

KK

F

PKKKW Bmd

svot =951.8 psi

o max

ySn = 44.1

Steering Ring

Material- 2024-T4 Aluminum, Yield Strength=47000 psi, Modulus of

Elasticity=10.4E6 psi, Poisson’s Ratio=.333

Max Bending Stress

o V

HW t 33000

= 39.3 lbf

o Ko= 1.25 - Overload Factor, based on light shocks encountered

o Kv= 1.10 - Dynamic Factor, based on quality and velocity of gears

o Ks= 1 - Size Factor

o Pd= 3.125” – Pitch diameter

o F= .125” – face width

o Km= 1.8 – Load-Distribution factor, based on geometry

o KB= 1 – Rim Thickness factor, based on geometry

o J= .4- Geometry factor, based on number of teeth of gears

Page 9: Shaft Stress Calculations - EDGEedge.rit.edu/edge/P07202/public/Mechanical/Documentation... · Shaft Stress Calculations Shaft 1 (Diameter=3 ... 1 = 2.25E12 cycles to failure Shaft

o J

KK

F

PKKKW Bmd

svot = 3996.0 psi

o max

ySn = 10.5

Miter Gears (Calculated using ANSI standards)

Both Miters (At max torque)

Material- Medium Carbon Steel, Yield Strength=76900 psi

Max Bending Stress

o Pd= 1.25” – Pitch diameter

o

o d

t

P

TW

2= 84.7 lbf

o Ko= 1.25 - Overload Factor, based on light shocks encountered

o Kv= 1 - Dynamic Factor, based on quality and velocity of gears

o Ks= .5 - Size Factor

o F= .27” – face width

o Km= 1.10 – Load-Distribution factor, based on geometry

o J= 0.175- Geometry factor, based on number of teeth of gears

o Kx= 1, Lengthwise curvature factor

o JK

KKKKP

F

W

x

msvod

t

=14922.2 psi

o max

ySn = 5.15

Both Miters (At max speed)

Material- Medium Carbon Steel, Yield Strength=76900 psi

Max Bending Stress

o Pd= 1.25” – Pitch diameter

o

o d

t

P

TW

2= 4 lbf

o Ko= 1.25 - Overload Factor, based on light shocks encountered

o Kv= 1.28 - Dynamic Factor, based on quality and velocity of gears

o Ks= .5 - Size Factor

o F= .27” – face width

o Km= 1.10 – Load-Distribution factor, based on geometry

o J= 0.175- Geometry factor, based on number of teeth of gears

o Kx= 1, Lengthwise curvature factor

o JK

KKKKP

F

W

x

msvod

t

=901.6 psi

o max

ySn = 85.3

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Forces

o Knowing max torque on miter (9.63 N-m), we can find the max tangential

force by dividing by half the pitch diameter=> Ftan=606.6 N

o = 20 degress -pressure angle

o d= 45 degrees

o cos

tanFFn =645.5 N

o sin

1nF

F =220.8 N

o dFFF radialaxial sin1 =156.1 N

Retaining Rings

On 3/8” shaft

o Ring can withstand 542.7 N of axial force

o Miter gear provides axial load= 156.1 N

o Factor of safety= 3.48

On 1/2” shaft

o Ring can withstand 542.7 N of axial force

o Miter gear provides axial load= 156.1 N

o Factor of safety= 3.48

On 3/4” shaft

o Ring can withstand 631.6 N of axial force

o Axial load is from turning

Assume wheel instantaneously turns 90 degrees, the max force that

can be applied axially would be equivalent to the frictional force

WFF frictionaxial =235.4 N (assuming =.6)

o Factor of safety= 2.68

Mechanical Brake

Max Temperature

Assuming all kinetic energy is converted directly into heat energy,

TCmvm vplatevehveh

22/1

Assume emergency brake will not be used continuously, but rather for one cycle

during the emergency

Assume initial temperature of 23 ° Celcius

Solving the above equation for Tfinal we find it to be 38.9 °Celcius

Heat Dissipation

Assuming Free Convection, the time required for heat dissipation can be

calculated

Utilizing the properties of air at room temperature, the Rayleigh number, Nusselt

number, and convection heat transfer coefficient can be calculated

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Using this information the heat transfer rate is determined

q

Et gives the time to dissipate the heat (4.8 minutes)

This resultant was later verified by the manufacturer of the brake

Keys

On 3/8” Shaft

Key is High carbon steel, Yield Strength 427 MPa, 3/32” square

Knowing the diameter of and torque on the shaft, the shear force on the key can

be calculated (2024.1 N)

Assuming a factor of safety of 4, the required length of the key is calculated

(.63”)

On 1/2” Shaft

Key is High carbon steel, Yield Strength 427 MPa, 1/8” square

Knowing the diameter of and torque on the shaft, the shear force on the key can

be calculated (1518.1 N)

Assuming a factor of safety of 4, the required length of the key is calculated

(.35”)

On 3/4” Shaft

Key is High carbon steel, Yield Strength 427 MPa, 3/16” square

Knowing the diameter of and torque on the shaft, the shear force on the key can

be calculated (4048.3 N)

Assuming a factor of safety of 4, the required length of the key is calculated

(.63”)

Keyways

Keyway analysis was done using Cosmos FEA software

By utilizing shaft diameters and torques, forces on keyway surfaces were

calculated and input into the program

Factor of Safety

o Driving Miter=16

o Driven Miter=15

o Driving Pulley=3.4

o Driven Pulley=8.4

o Driven Spur=8.1

o Wheel=1.8, but in reality, failure would result in the slip of a pressed

insert, rather than physical failure of the wheel

Set Screws

To connect spur gear to 5/16” drive motor shaft

By choosing a screw size and quantity (2- #8’s), the maximum force at the shaft

surface can be calculated (3425.1 N)

Page 12: Shaft Stress Calculations - EDGEedge.rit.edu/edge/P07202/public/Mechanical/Documentation... · Shaft Stress Calculations Shaft 1 (Diameter=3 ... 1 = 2.25E12 cycles to failure Shaft

The torque and diameter of the shaft is used to determine the actual force seen at

this shaft surface (1214.5 N)

By comparing these two values the factor of safety is determined (2.82)

To connect spur gear to 8mm steering motor shaft

By choosing a screw size and quantity (2-#6’s), the maximum force at the shaft

surface can be calculated (2224.1 N)

The torque and diameter of the shaft is used to determine the actual force seen at

this shaft surface (234.6 N)

By comparing these two values the factor of safety is determined (9.5)

Timing Belt and Pulleys

Utilizing MITCalc simulation software and inputting various parameters

including distance between centers, power applied to belt, operating

speeds, and other operating conditions a belt type and specific model was

selected

From this the 5M Powergrip GT2 belt was chosen and matched with

pulleys of 18 and 72 teeth

The selection of these parts was also verified with an engineer at the

supplier sdp-si.com

Bearings

C10 = Catalog Load Rating (lbf)

LR = Rating Life (hrs)

nR = Rating Speed (RPM)

FD = Desired Radial Load (lbf)

LD = Desired Life (hrs)

nD = Desired Speed (RPM)

FR = Radial Force (lbf)

FA = Axial Force (lbf)

Fe = Equivalent Radial Load (lbf)

C0 = Static Load Rating (lbf)

X2 = Factor dependent on bearing geometry

Y2 = Factor dependent on bearing geometry

V = Rotation Factor

a = 3 (ball bearing)

e = abscissa

Lower Drive Bearing

C10 (lbs) 1171 Upper Drive Bearing Center Bearing

LR * nR 1.0E+06 C10 (lbs) 1187 C10 (lbs) 691

FD (lbs) 44.125 LR * nR 1.0E+06 LR * nR 1.0E+06

nD (RPM) 5.0E+02 Fe (lbs) 84.6 Fe (lbs) 70.6

a 3 nD (RPM) 2000 nD (RPM) 4000

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ARe

D

RR

a

D

D

FYVFXF

n

nL

F

CL

22

10 *

LD (hrs) 3.74E+07 FA (lbs) 35.1 FA (lbs) 35.1

LD (years) 4267 FR (lbs) 35.1 FR (lbs) 35.1

a 3 a 3

Steering Bearing V 1 V 1

C10 (lbs) 300 e 0.24 e 0.3

LR * nR 1.0E+06 X2 0.56 X2 0.56

FD (lbs) 10 Y2 1.85 Y2 1.45

nD (RPM) 340 LD (hrs) 1.38E+06 LD (hrs) 2.34E+05

a 3 LD (years) 158 LD (years) 27

LD (hrs) 7.94E+07

LD (years) 9065

Screws

Bolts connecting Yoke to Turntable

Bolt type: 4 * 10-32 (SAE)

Torque applied to the turntable

T= 2.38 N-m

Converted ASTM

T = 21 lb-in

Resultant load on each bolt

lbin

inlbr

TV 108.8

59.2

1*21

inlbTM 21

Primary Shear Load per Bolt is

lbn

VF 027.2

4

108.8'

Since the secondary shear Forces are equal we have

lbr

M

r

MrF 027.2

59.2*4

21

44''

2

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The resultant force is

lbFr 867.2

Fr = Fa = Fb = Fc = Fd = 2.867lb

Maximum Shear Stress

As = 0.155

psiA

F

s

r 497.18155.

867.2

Bolts connecting Brake to Brake plate

Bolt type: 4 * 8-32 (SAE)

Torque applied to the turntable

T = 15 lb-in

Resultant load on each bolt

lbin

inlbr

TV 33.13

125.1

1*15

inlbTM 15

Primary Shear Load per Bolt is

lbn

VF 33.3

4

33.13'

Since the secondary shear Forces are equal we have

lbr

M

r

MrF 33.3

125.1*4

15

44''

2

The resultant force is

lbFr 714.4

Page 15: Shaft Stress Calculations - EDGEedge.rit.edu/edge/P07202/public/Mechanical/Documentation... · Shaft Stress Calculations Shaft 1 (Diameter=3 ... 1 = 2.25E12 cycles to failure Shaft

Fr = Fa = Fb = Fc = Fd = 4.714 lb

Maximum Shear Stress

As = .0992

psiA

F

s

r 9.280992.

867.2

Yoke

Yoke stress analysis was done using Cosmos FEA software

Loading

o Weight vertically loads lower bearing holes (196.2 N each)

o Turning force loads inside wall (158.3 N)

o Driven Miter axial force loads inside wall (156 N)

o Driven Miter radial force loads upper bearing holes

Page 16: Shaft Stress Calculations - EDGEedge.rit.edu/edge/P07202/public/Mechanical/Documentation... · Shaft Stress Calculations Shaft 1 (Diameter=3 ... 1 = 2.25E12 cycles to failure Shaft

o Driving Miter axial force loads upward on top plate

Minimum factor of safety= 20

Brake Plate

Brake plate stress analysis was done using Cosmos FEA software

Loading

o Outside edge was fixed, as it is welded to the motor mount assembly

o Each brake mounting hole was loaded with a force corresponding to the

brake’s torque output and the holes distance from center

Minimum factor of safety= 200

Turntable

Capable of withstanding 750 lbs, or 340 kg

Actual weight is about 40 kg per module

Factor of Safety= 8.5

Page 17: Shaft Stress Calculations - EDGEedge.rit.edu/edge/P07202/public/Mechanical/Documentation... · Shaft Stress Calculations Shaft 1 (Diameter=3 ... 1 = 2.25E12 cycles to failure Shaft

Figure X: Shaft Stress and Fatigue Strength Calculations

Figure X: Drive Motor Spur Gear Stress Calculation

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Figure X: Miter Gear Stress and Force Calculation

Figure X: Retaining Ring Calculations Figure X: Impact Calculations

Figure X: Brake Temperature and Heat Dissipation Calculations

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Figure X: Key and Set Screw Analysis

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Figure X: Timing Belt and Pulley Analysis

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Figure X: Driven Miter Gear Keyway Analysis

Figure X: Driving Miter Gear Keyway Analysis

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Figure X: Driven Pulley Keyway Analysis

Figure X: Driving Pulley Keyway Analysis (Representation)

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Figure X: Driven Spur Gear Keyway Analysis

Figure X: Wheel Keyway Analysis (Representation)

Note: Actual wheel utilizes press fit keyway insert, thus failure during stall will result in

slip of this insert, rather than the physical failure of a mechanical part

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Figure X: Yoke Displacement